COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 200 (Super King Air) Series Aeroplanes
AD/BEECH 200/19 Main Landing Gear Torque Tubes 7/77
Applicability: All models 200 with S/Nos. BB-2 to BB-41, BB-43 to BB-121, BB-123 to BB-130, BB-132 to BB-137 and BB-139 to BB-157.
Requirement: Action in accordance with Beechcraft SI No 0891. Compliance: Within 100 hours time in service after 31 July 1977.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, include specific regulations to ensure the safety and airworthiness of aircraft. One such regulation is found in Part 39, which addresses the issuance of airworthiness directives. Among these, AD/BEECH 200/19 pertains to the Beechcraft 200 (Super King Air) series aeroplanes, focusing on the main landing gear torque tubes. This directive was introduced to address potential safety issues related to the specified models of these aircraft. The objective is to ensure that all applicable aircraft meet stringent safety standards to protect passengers and crew. Compliance with this directive is mandatory for specified serial numbers, requiring corrective actions within 100 hours of time in service following the directive's effective date of 31 July 1977.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, mandates certain safety requirements for Beechcraft 200 (Super King Air) series aeroplanes. The regulation applies to all models 200 with specific serial numbers, targeting the main landing gear torque tubes. The requirement necessitates compliance with Beechcraft Service Information No. 0891, which must be implemented within 100 hours of time in service following 31 July 1977. This regulation applies to aircraft owners, operators, and maintenance personnel within the Commonwealth of Australia, ensuring adherence to civil aviation safety standards. The scope of this directive is limited to the specified models and serial numbers of the Beechcraft 200 series aeroplanes, and any exclusions or exemptions are not detailed within this directive. The regulation extends its application through subordinate instruments such as service information notices issued by the aircraft manufacturer, Beechcraft, to provide detailed compliance instructions.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain detailed provisions for the safety and maintenance of aircraft, including the Beechcraft 200 (Super King Air) series aeroplanes. Under this part, the regulation AD/BEECH 200/19 addresses the requirement for the main landing gear torque tubes on certain models of the Beechcraft 200 series aeroplanes (section 105.10). This airworthiness directive pertains to aircraft with specific serial numbers: BB-2 to BB-41, BB-43 to BB-121, BB-123 to BB-130, BB-132 to BB-137, and BB-139 to BB-157 (section 105.12).
The directive mandates that action be taken in accordance with Beechcraft Service Instruction (SI) No 0891 to address the identified issue with the main landing gear torque tubes. Compliance with this directive must be achieved within 100 hours of time in service after 31 July 1977 (section 105.14). This means that the specified maintenance action must be completed before the aircraft accumulates 100 hours of operation following the specified date.
Entities and individuals governed by these regulations are required to ensure that the prescribed maintenance action on the main landing gear torque tubes is performed as stipulated. This involves following the detailed instructions laid out in the Beechcraft SI No 0891, which likely includes inspection, repair, or replacement procedures. Failure to comply with these requirements could result in serious safety risks, including potential structural failure during flight, which could lead to catastrophic outcomes.
Should any entity or individual fail to adhere to the provisions outlined in this airworthiness directive, they may be subject to enforcement actions. While the specific penalties are not detailed in the provided text, under the broader Civil Aviation Regulations, non-compliance can lead to both civil and criminal penalties. Civil penalties can include fines, while criminal penalties may involve imprisonment, reflecting the critical importance of adhering to these safety directives. It is essential for those responsible for the maintenance of these aircraft to ensure full compliance to avoid any legal repercussions.